Aluminum alloy material, and conductive member, battery member, fastening component, spring component, and structural component including the aluminum alloy material

ABSTRACT

An aluminum alloy material is an aluminum alloy material having an alloy composition consisting of 0.2 to 1.8% by mass of Mg, 0.2 to 2.0% by mass of Si, 0.01 to 1.50% by mass of Fe, 0.06 to 2% by mass in total of at least one selected from Cu, Ag, Zn, Ni, Co, Au, Mn, Cr, V, Zr, and Sn, with the balance containing Al and inevitable impurities. The aluminum alloy material has a fibriform metallographic structure where crystal grains extend so as to be aligned in one direction. In a cross section parallel to the one direction, an average value of a size perpendicular to a longitudinal direction of the crystal grains is 270 nm or less.

CROSS REFERENCE TO RELATED APPLICATIONS

This is a continuation application of International Patent Application No. PCT/JP2017/025212 filed Jul. 11, 2017, which claims the benefit of Japanese Patent Application No. 2016-138842 filed Jul. 13, 2016, the full contents of all of which are hereby incorporated by reference in their entirety.

BACKGROUND Technical Field

The present disclosure relates to an aluminum alloy material having a high strength. Such an aluminum alloy material is used for a wide range of applications (for example, a conductive member, a battery member, a fastening component, a spring component, and a structural component).

Description of the Related Art

In recent years, with the diversification of the shapes of metal members, a technique is being widely studied which causes a metal powder to be sintered using electron beams or lasers or the like, thereby molding a three-dimensional structure having a desired shape. However, such a technique uses the metal powder, and has for example the following problem: an excessively fine metal powder is apt to explode.

Therefore, these days, a technique is being developed which molds a three-dimensional structure according to a method for knitting, weaving, tying, jointing, or connecting metal fine wires. The consideration of such a method is advanced, for example, as Wire-Woven Cellular Materials, and the application of the method to a battery component, a heat sink, and an impact absorption member or the like is expected.

An iron-based or copper-based wire rod has been widely used as the metal fine wire. These days, there is considered substitution of the iron-based or copper-based metal material to an aluminum-based material having a small specific gravity, a large thermal expansion coefficient, comparatively good electrical and heat conductivities, and excellent corrosion resistance, particularly having a small elastic coefficient, and flexibly elastically deformed as compared with the iron-based or copper-based metal material.

However, a pure aluminum material has the following problem: it has a lower strength than that of the iron-based or copper-based metal material. A 2000 or 7000-series aluminum alloy material which is an aluminum-based alloy material having a comparatively high strength has the following problem: it has poor corrosion resistance and stress corrosion cracking resistance.

Therefore, these days, there is widely used a 6000-series aluminum alloy material which contains Mg and Si and has excellent electrical and heat conductivities, and excellent corrosion resistance. Such a 6000-series aluminum alloy material has a higher strength in aluminum-based alloy materials, but it does not have a sufficient strength, whereby a further improvement in a strength is desired.

On the other hand, a method according to crystallization of an aluminum alloy material containing an amorphous phase (Japanese Patent Application Publication No. 5-331585), a method for forming fine crystal grains according to the ECAP method (Japanese Patent Application Publication No. 9-137244), a method for forming fine crystal grains according to cold working at a temperature equal to or less than room temperature (Japanese Patent Application Publication No. 2001-131721), and a method for dispersing carbon nanofibers (Japanese Patent Application Publication No. 2010-159445) or the like are known as a method for improving the strength of the aluminum alloy material. However, the methods manufacture aluminum alloy materials having small sizes, which make it difficult to industrially put the aluminum alloy materials to practical use.

A method for controlling a rolling temperature to obtain an Al—Mg-based alloy having a fine structure is disclosed in Japanese Patent Application Publication No. 2003-027172. The method has excellent industrial mass productivity, but a further improvement in a strength is required.

SUMMARY

The present disclosure is related to providing an aluminum alloy material which can serve as a substitute for an iron-based or copper-based metal material and has a high strength, and providing a conductive member, a battery member, a fastening component, a spring component, and a structural component including the aluminum alloy material.

According to a first aspect of the present disclosure, an aluminum alloy material has an alloy composition consisting of 0.2 to 1.8% by mass of Mg, 0.2 to 2.0% by mass of Si, 0.01 to 1.50% by mass of Fe, 0.06 to 2% by mass in total of at least one selected from Cu, Ag, Zn, Ni, Co, Au, Mn, Cr, V, Zr, and Sn, with the balance containing Al and inevitable impurities. The aluminum alloy material has a fibriform metallographic structure where crystal grains extend so as to be aligned in one direction. In a cross section parallel to the one direction, an average value of a size perpendicular to a longitudinal direction of the crystal grains is 270 nm or less.

Further, it is preferable that an aspect ratio of the crystal grains is in excess of 10.

Further, it is preferable that the aluminum alloy material has a Vickers hardness (HV) of 125 to 250.

According to a second aspect of the present disclosure, a conductive member includes the aluminum alloy material according to the present disclosure.

According to a third aspect of the present disclosure, a battery member includes the aluminum alloy material according to the present disclosure.

According to a fourth aspect of the present disclosure, a fastening component includes the aluminum alloy material according to the present disclosure.

According to a fifth aspect of the present disclosure, a spring component includes the aluminum alloy material according to the present disclosure.

According to a sixth aspect of the present disclosure, a structural component includes the aluminum alloy material according to the present disclosure.

The present disclosure can provide an aluminum alloy material having excellent heat resistance and a high strength comparable to that of an iron-based or copper-based metal material. Furthermore, the present disclosure can provide a conductive member, a battery member, a fastening component, a spring component, and a structural component including the aluminum alloy material.

BRIEF DESCRIPTION OF DRAWINGS

FIG. 1 A perspective view schematically showing the situation of the metallographic structure of an aluminum alloy material according to the present disclosure.

FIG. 2 A graph showing the relationship between the degree of working and tensile strength of each of pure aluminum, pure copper, and an aluminum alloy material according to the present disclosure.

FIG. 3 A STEM image showing the situation of a metallographic structure in a cross section parallel to a working direction X of an aluminum alloy material according to the Examples.

DETAILED DESCRIPTION

Hereinafter, preferred embodiments of an aluminum alloy material of the present disclosure are described in detail. The aluminum alloy material according to the present disclosure has an alloy composition consisting of 0.2 to 1.8% by mass of Mg, 0.2 to 2.0% by mass of Si, 0.01 to 1.50% by mass of Fe, 0.06 to 2% by mass in total of at least one selected from Cu, Ag, Zn, Ni, Co, Au, Mn, Cr, V, Zr, and Sn, with the balance containing Al and inevitable impurities. The aluminum alloy material has a fibriform metallographic structure where crystal grains extend so as to be aligned in one direction. In a cross section parallel to the one direction, the average value of a size perpendicular to the longitudinal direction of the crystal grains is 270 nm or less.

Herein, the “crystal grains” refer to portions surrounded by orientation difference boundaries. Here, the “orientation difference boundary” refers to a boundary where contrast discontinuously changes in a case in which a metallographic structure is observed by scanning transmission electron microscopy (STEM). The size perpendicular to the longitudinal direction of the crystal grains corresponds to the interval of the orientation difference boundaries.

The aluminum alloy material according to the present disclosure has a fibriform metallographic structure where crystal grains extend so as to be aligned in one direction. Here, FIG. 1 shows a perspective view schematically showing the situation of the metallographic structure of the aluminum alloy material according to the present disclosure. As shown in FIG. 1, the aluminum alloy material of the present disclosure has a fibriform structure where crystal grains 10 each having an elongated shape extend so as to be aligned in one direction X. The crystal grains each having an elongated shape are completely different from conventional fine crystal grains and flat crystal grains each merely having a large aspect ratio. Specifically, the crystal grains of the present disclosure each have an elongated shape as with a fiber, and the average value of a size t perpendicular to a longitudinal direction X thereof is 270 nm or less. The fibriform metallographic structure where the fine crystal grains extend so as to be aligned in one direction can be said to be a novel metallographic structure which is not included in a conventional aluminum alloy.

The aluminum alloy material of the present disclosure has the fibriform metallographic structure where the crystal grains extend so as to be aligned in one direction, and in the cross section parallel to the one direction, the average value of the size perpendicular to the longitudinal direction of the crystal grains is controlled to 270 nm or less, whereby a high strength (for example, a tensile strength of 480 MPa or more and a Vickers hardness (HV) of 125 or more) comparable to that of an iron-based or copper-based metal material can be attained.

The fine crystal grain size leads directly to an effect of improving grain boundary corrosion, an effect of improving fatigue characteristics, an effect of reducing the roughness of a surface after plastic working, and an effect of reducing sagging and burr during shearing working, or the like in addition to an improvement in a strength, which provides effects of generally improving the functions of the material.

(1) Alloy Composition

The alloy composition of the aluminum alloy material of the present disclosure and the effects of the alloy composition are described.

<Mg: 0.2 to 1.8% by Mass>

Mg (magnesium) has an effect of strengthening by forming a solid solution in an aluminum matrix, and has an effect of improving a tensile strength by a synergistic effect with Si. In a case where it forms a Mg—Si cluster as a solute atom cluster, it is an element having an effect of improving a tensile strength and an elongation. However, in a case where a Mg content is less than 0.2% by mass, the above function effects are insufficient. In a case where the Mg content is in excess of 1.8% by mass, a crystallized material is formed, which causes deterioration in workability (wire drawing workability and bending workability or the like). Therefore, the Mg content is 0.2 to 1.8% by mass, and preferably 0.4 to 1.0% by mass.

<Si: 0.2 to 2.0% by Mass>

Si (silicon) has an effect of strengthening by forming a solid solution in an aluminum matrix, and has an effect of improving a tensile strength and bending fatigue resistance by a synergistic effect with Mg. In a case where it forms a Mg—Si cluster or an Si—Si cluster as a solute atom cluster, it is an element having an effect of improving a tensile strength and an elongation. However, in a case where an Si content is less than 0.2% by mass, the above function effects are insufficient. In a case where the Si content is in excess of 2.0% by mass, a crystallized material is formed, which causes deterioration in workability. Therefore, the Si content is 0.2 to 2.0% by mass, and preferably 0.4 to 1.0% by mass.

<Fe: 0.01 to 1.50% by Mass>

Fe (iron) is an element which contributes to refinement of crystal grains by forming an Al—Fe based intermetallic compound and provides an improved tensile strength. Here, the intermetallic compound refers to a compound composed of two or more kinds of metals. Fe dissolves in Al only by 0.05% by mass at 655° C., and even less at room temperature. Accordingly, the remaining Fe which cannot dissolve in Al is crystallized or precipitated as an intermetallic compound such as Al—Fe, Al—Fe—Si, or Al—Fe—Si—Mg. An intermetallic compound mainly composed of Fe and Al as exemplified by the above-described intermetallic compounds is herein referred to as an Fe-based compound. This intermetallic compound contributes to the refinement of crystal grains and provides an improved tensile strength. Fe has, also by Fe which has dissolved in Al, an effect of providing an improved tensile strength. In a case where an Fe content is less than 0.01% by mass, these function effects are insufficient. In a case where the Fe content is in excess of 1.50% by mass, a crystallized material increases, which causes deterioration in workability. Here, the crystallized material refers to an intermetallic compound occurring during the casting solidification of an alloy. Therefore, the Fe content is 0.01 to 1.50% by mass, and preferably 0.05 to 0.80% by mass. In a case where a cooling speed during casting is slow, the dispersion of the Fe-based compound is sparse, which causes the increased degree of a negative effect. Therefore, the Fe content is more preferably less than 1.00% by mass, and still more preferably less than 0.60% by mass.

<At Least One or More Selected From Cu, Ag, Zn, Ni, Co, Au, Mn, Cr, V, Zr, and Sn: 0.06 to 2% by Mass in Total>

Each of Cu (copper), Ag (silver), Zn (zinc), Ni (nickel), Co (cobalt), Au (gold), Mn (manganese), Cr (chromium), V (vanadium), Zr (zirconium), and Sn (stannum) is an element which provides improved heat resistance. Only any one type of these components may be contained singly, or the components may be contained in combination of two or more types.

Examples of a mechanism in which the components provide improved heat resistance include a mechanism which reduces the energy of a crystal grain boundary since the difference between the atomic radius of each of the components and the atomic radius of aluminum is large, a mechanism which reduces the mobility of the grain boundary in a case in which each of the components enters into the grain boundary since the diffusion coefficient of the component is large, and a mechanism which delays a diffusion phenomenon since the interaction of the components with holes is large to trap the holes. These mechanisms are considered to act synergistically.

Considering corrosion resistance in a case of being particularly used in a corrosion environment, any one or more selected from Zn, Ni, Co, Mn, Cr, V, Zr, and Sn is preferably contained. Furthermore, in a case in which the total of the contents of the components is less than 0.06% by mass, the function effect is insufficient. In a case in which the total of the contents of the components are in excess of 2% by mass, workability decreases. Therefore, the total of the contents of at least one or more selected from Cu, Ag, Zn, Ni, Co, Au, Mn, Cr, V, Zr, and Sn is 0.06 to 2% by mass, and preferably 0.3 to 1.2% by mass.

<Balance: Al and Inevitable Impurities>

The balance, i.e., components other than those described above, includes Al (aluminum) and inevitable impurities. Herein, the inevitable impurities mean impurities contained by an amount which may be contained inevitably during a manufacturing process. Since the inevitable impurities may cause a decrease in conductivity depending on the content thereof, it is preferable to suppress the content of the inevitable impurities to some extent considering the decrease in the conductivity. Examples of components which are inevitable impurities include B (boron), Ti (titanium), Bi (bismuth), Pb (lead), Ga (gallium), and Sr (strontium). The upper limit of the content of each of the components may be 0.05% by mass or less, and the total amount of the components may be 0.15% by mass or less.

Such an aluminum alloy material can be obtained by combining and controlling alloy compositions and manufacturing processes. Hereinafter, a suitable manufacturing method of the aluminum alloy material of the present disclosure is described.

(2) Manufacturing Method of Aluminum Alloy Material According to One Example of Present Disclosure

Such an aluminum alloy material according to one example of the present disclosure particularly attains an improvement in a strength by introducing a crystal grain boundary into an Al—Mg—Si—Fe-based alloy at a high density. Therefore, an approach to an improvement in a strength is largely different from that in a method for precipitation-hardening a Mg—Si compound which has been generally performed in a conventional aluminum alloy material.

In a preferable manufacturing method of the aluminum alloy material of the present disclosure, an aluminum alloy material having a predetermined alloy composition is subjected to cold working [1] at a degree of working of 4 or more as last working without subjecting the aluminum alloy material to an aging precipitation heat treatment [0]. Refine annealing [2] may be performed after the cold working [1] if needed. Hereinafter, the manufacturing method is described in detail.

Usually, in a case in which deformation stress is applied to a metal material, crystal slip occurs as the elementary step of the deformation of a metal crystal. The metal material in which the crystal slip is apt to occur has small stress required for deformation, whereby it can be said to be have a low strength. Therefore, it is important to suppress the crystal slip which occurs in the metallographic structure in order to provide the improvement in the strength of the metal material. Examples of the prevention factor of such crystal slip include the existence of the crystal grain boundary in the metallographic structure. Such a crystal grain boundary can prevent the crystal slip from spreading in the metallographic structure in a case in which the deformation stress is applied to the metal material. As a result, the strength of the metal material is improved.

Therefore, it is considered that, in order to improve the strength of the metal material, the crystal grain boundary is desirably introduced at a high density into the metallographic structure. Here, the formation mechanism of the crystal grain boundary is considered to be the division of the metal crystal involving the following deformation of the metallographic structure, for example. Usually, in a polycrystalline material, the difference between the orientations of adjacent crystal grains, and the space distribution of distortion between the vicinity of a surface layer brought into contact with a working tool and the inside of bulk cause a stress state to be in a complicated multiaxial state. Under these influences, a crystal grain which is in a single orientation before deformation is divided in a plurality of orientations with the deformation, and a crystal grain boundary is formed between the divided crystals.

However, the formed crystal grain boundary has surface energy in a structure deviated from the closest packed atomic arrangement of usual twelve coordination. Therefore, it is considered that, in the usual metallographic structure, in a case in which the crystal grain boundary has a given density or more, the increased internal energy serves as a driving force, whereby dynamic or static recovery and recrystallization occur. Therefore, usually, it is considered that the increase and reduction of the crystal grain boundary simultaneously occur even if the amount of deformation is increased, whereby a grain boundary density is saturated.

Such a phenomenon coincides with also the relationship between a degree of working and a tensile strength in pure aluminum or pure copper which is a conventional metallographic structure. FIG. 2 shows a graph of the relationship between the degree of working and tensile strength of each of pure aluminum, pure copper, and the aluminum alloy material according to the present disclosure.

As shown in FIG. 2, pure aluminum or pure copper which is a usual metallographic structure has an improved tensile strength (hardening) at a comparatively low degree of working, but as the degree of working increases, the amount of hardening tends to be saturated. Here, it is considered that the degree of working corresponds to the amount of deformation applied to the metallographic structure, and the saturation of the amount of hardening corresponds to the saturation of the grain boundary density.

On the other hand, it was found that the aluminum alloy material of the present disclosure is continuously hardened even if the degree of working increases, and the strength of the aluminum alloy material continuously increases with working. This is considered to be because the aluminum alloy material of the present disclosure has the above alloy composition, and particularly, predetermined amounts of Mg and Si are compositely added to the aluminum alloy material, whereby the increase in the internal energy can be suppressed even if the crystal grain boundary has a given density or more in the metallographic structure. This is considered to make it possible to prevent recovery and recrystallization in the metallographic structure, and effectively increase the crystal grain boundary in the metallographic structure.

The mechanism of the improvement in the strength provided by the composite addition of Mg and Si is not necessarily clear. However, the mechanism is considered to be based on the following (i) and (ii): (i) by combining and using a Mg atom having a greater atomic radius than that of an Al atom and an Si atom having a smaller atomic radius than that of the Al atom, the atoms are always filled densely (arranged) in the aluminum alloy material; and (ii) by causing divalent Mg and tetravalent Si to coexist with respect to a trivalent Al atom, a trivalent state can be formed in the entire aluminum alloy material, which attains valence stability, whereby the increase in the internal energy involving working can be effectively suppressed.

In the present disclosure, the degree of working in the cold working [1] is set to 4 or more. In particular, working at a large degree of working makes it possible to prompt the division of the metal crystal involving the deformation of the metallographic structure, and to introduce the crystal grain boundary into the aluminum alloy material at a high density. As a result, the grain boundary of the aluminum alloy material is strengthened to largely improve the strength. Such a degree of working is set to preferably 5 or more, more preferably 6 or more, and still more preferably 7 or more. The upper limit of the degree of working is not particularly prescribed, and usually 15 or less.

A degree of working η is represented by the following formula (1) in a case in which a cross-sectional area before working is taken as s1, and a cross-sectional area after working is taken as s2 (s1>s2).

Degree of working (non-dimension): η=ln(s1/s2)   (1)

A working rate is preferably set to 98.2% or more, and more preferably 99.8% or more. A working rate R is represented by the following formula (2) using the above s1 and s2.

Working rate (%): R={(s1−s2)/s1}×100   (2)

A working method may be appropriately selected according to the intended shape (a wire bar, a plate, a strip, a foil or the like) of the aluminum alloy material, and examples thereof include a cassette roller die, groove roll rolling, round wire rolling, drawing working using a die or the like, and swaging. Various conditions (kind of lubricating oil, working speed, and working heat generation or the like) in the above working may be appropriately adjusted in a known range.

The aluminum alloy material is not particularly limited as long as it has the above alloy composition. For example, it is possible to appropriately select and use an extruded material, an ingot material, a hot-rolled material, and a cold-rolled material or the like according to the purpose of use.

In the present disclosure, the aging precipitation heat treatment [0] which has been conventionally performed before the cold working [1] is not performed. Such an aging precipitation heat treatment [0] usually retains the aluminum alloy material at 160 to 240° C. for 1 minute to 20 hours, to prompt precipitation of a Mg—Si compound. However, in a case in which the aluminum alloy material is subjected to such an aging precipitation heat treatment [0], the above cold working [1] at the high degree of working cannot be performed since working cracks occur in the material. Since a high aging temperature causes an overaging state, the working cracks may not occur even in the above cold working [1] at the high degree of working. However, in this case, Mg and Si are discharged from an Al matrix phase as a Mg—Si compound, whereby the stability of the grain boundary remarkably deteriorates.

In the present disclosure, the refine annealing [2] may be performed after the cold working [1] for the purposes of release of residual stress and an improvement in an elongation. In a case in which the refine annealing [2] is performed, a treatment temperature is set to 50 to 160° C. In a case in which the treatment temperature of the refine annealing [2] is less than 50° C., the above effects are less likely obtained. In a case in which the treatment temperature is in excess of 160° C., recovery or recrystallization causes the growth of the crystal grains to occur, which causes a decrease in the strength. The retention time of the refine annealing [2] is preferably 1 to 48 hours. The various conditions of such a heat treatment can be appropriately adjusted according to the kind and amount of inevitable impurities, and the solid solution/precipitation state of the aluminum alloy material.

In the present disclosure, as described above, the aluminum alloy material is subjected to working at a high degree of working according to a method such as drawing using a die, or rolling. Therefore, as a result, an elongated aluminum alloy material is obtained. On the other hand, a conventional method for manufacturing an aluminum alloy material such as powder sintering, compression torsion working, high pressure torsion (HPT), forge working, or equal channel angular pressing (ECAP) makes it difficult to provide the elongated aluminum alloy material. The aluminum alloy material of the present disclosure is preferably manufactured so as to have a length of 10 m or more. The upper limit of the length of the aluminum alloy material during manufacturing is not particularly provided, and preferably 6000 m or less in consideration of workability or the like.

Since it is effective to increase the degree of working for providing fine crystal grains as described above, the configuration of the present disclosure is likely to be attained as the diameter of the aluminum alloy material of the present disclosure is smaller, particularly, in a case in which the aluminum alloy material is produced as a wire bar, or as the thickness of the aluminum alloy material is smaller in a case in which the aluminum alloy material is produced as a plate or a foil.

In particular, in a case in which the aluminum alloy material of the present disclosure is a wire bar, the wire bar has a wire diameter of preferably 1 mm or less, more preferably 0.5 mm or less, still more preferably 0.1 mm or less, and particularly preferably 0.07 mm or less. The upper limit is not particularly provided, and preferably 30 mm or less. The aluminum alloy wire bar of the present disclosure has one advantage that it can be used as a thin single wire.

As described above, the aluminum alloy material of the present disclosure is slimly or thinly worked. A plurality of aluminum alloy materials are prepared and joined to provide a large or thick product, which can also be used for the intended application. A known method can be used for the joining method, and examples thereof include pressure welding, welding, joining using an adhesive, and friction stirring joining. In a case in which the aluminum alloy material is the wire bar, a plurality of wire bars are bundled, and twisted to provide a twisted product, which can also be used for the intended application as an aluminum alloy twisted wire. The aluminum alloy material subjected to the cold working [1] may be subjected to working according to joining or twisting, and then subjected to the step of the refine annealing [2].

(3) Organizational Feature of Aluminum Alloy Material of Present Disclosure

The aluminum alloy material of the present disclosure manufactured by the above manufacturing method is obtained by introducing the crystal grain boundary at a high density into the metallographic structure. The aluminum alloy material of the present disclosure has the fibriform metallographic structure where the crystal grains extend so as to be aligned in one direction, and in the cross section parallel to the one direction, the average value of a size perpendicular to the longitudinal direction of the crystal grains is 270 nm or less. The aluminum alloy material has a non-conventional specific metallographic structure, whereby the aluminum alloy material can exhibit a particularly excellent strength.

The metallographic structure of the aluminum alloy material of the present disclosure is the fibriform structure, and the crystal grains each having an elongated shape extend in fiber forms so as to be aligned in one direction. Here, the “one direction” corresponds to the working direction of the aluminum alloy material. In a case in which the aluminum alloy material is the wire bar, the “one direction” corresponds to a wire drawing direction, for example. In a case in which the aluminum alloy material is a plate or a foil, the “one direction” corresponds to a rolling direction, for example. Particularly, the aluminum alloy material of the present disclosure exhibits a particularly excellent strength with respect to tensile stress parallel to the working direction.

The one direction preferably corresponds to the longitudinal direction of the aluminum alloy material. Specifically, as long as the aluminum alloy material is not divided into pieces so as to have a size shorter than a size perpendicular to the working direction, the working direction of the aluminum alloy material usually corresponds to the longitudinal direction.

In the cross section parallel to the one direction, the average value of a size perpendicular to the longitudinal direction of the crystal grains is 270 nm or less, more preferably 220 nm or less, still more preferably 170 nm or less, and particularly preferably 120 nm or less. In the fibriform metallographic structure where the crystal grains having a small diameter (size perpendicular to the longitudinal direction of the crystal grains) extend in one direction, the crystal grain boundary is formed at a high density. Such a metallographic structure makes it possible to effectively inhibit the crystal slip involving deformation, which makes it possible to attain a non-conventional high strength. The lower limit of the average value of a size perpendicular to the longitudinal direction of the crystal grains is preferably 50 nm or more from the viewpoint of preventing deterioration in ductility.

The size of the longitudinal direction of the crystal grains is not necessarily specified, and preferably 1200 nm or more, more preferably 1700 nm or more, and still more preferably 2200 nm or more. The aspect ratio of the crystal grains is preferably in excess of 10, and more preferably 20 or more. The upper limit of the aspect ratio of the crystal grains is preferably 2 million or less from the viewpoint of preventing deterioration in ductility.

(4) Characteristics of Aluminum Alloy Material of Present Disclosure

[Tensile Strength]

A tensile strength is measured according to JIS Z2241: 2011. Detailed measurement conditions are described in the column of Examples to be described below. In a case in which the aluminum alloy material of the present disclosure is particularly the wire bar, the aluminum alloy material has a tensile strength of preferably 480 MPa or more. This is a strength equivalent to that of a copper wire subjected to wire drawing working at a general high degree of working. The aluminum alloy material has a tensile strength of more preferably 520 MPa or more, still more preferably 560 MPa or more, particularly preferably 600 MPa or more, and yet still more preferably 640 MPa or more. The aluminum alloy material of the present disclosure having such a high strength can be used as substitution of a strong wire drawing worked material made of a thin copper alloy such as a Cu—Sn and Cu—Cr alloy. Such an aluminum alloy material can also be used as substitution of a steel-based or stainless-based material. The upper limit of the tensile strength of the aluminum alloy material of the present disclosure is not particularly limited, and 1000 MPa or less, for example. Since the aluminum alloy material of the present disclosure has excellent heat resistance, the aluminum alloy material can maintain the above high tensile strength even after heating.

[Vickers Hardness (HV)]

A Vickers hardness (HV) is a value measured according to JIS Z 2244: 2009. Detailed measurement conditions are described in the column of Examples to be described below. The Vickers hardness (HV) of a worked product which has been already turned into a component can be measured as follows: the worked product is disassembled; the cross section thereof is subjected to mirror polishing; and the Vickers hardness of the cross section is measured. In a case in which the aluminum alloy material of the present disclosure is particularly the wire bar, the Vickers hardness (HV) is preferably 125 or more. This is a strength equivalent to that of a copper wire subjected to general strong wire drawing working. The Vickers hardness (HV) of the aluminum alloy material is more preferably 140 or more, still more preferably 150 or more, particularly preferably 160 or more, and yet still more preferably 170 or more. The aluminum alloy material of the present disclosure having such a high strength can be used as substitution of a strong wire drawing worked material made of a thin copper alloy such as a Cu—Sn or Cu—Cr alloy. Such an aluminum alloy material can also be used as substitution of a steel-based or stainless-based material. The upper limit of the Vickers hardness (HV) of the aluminum alloy material of the present disclosure is not particularly limited, and 300 or less, for example, and preferably 250 or less.

(5) Application of Aluminum Alloy Material of Present Disclosure

The aluminum alloy material of the present disclosure can be directed to all the applications in which an iron-based material, a copper-based material, and an aluminum-based material are used. Specifically, the aluminum alloy material can be suitably used as a conductive member such as an electric wire or a cable, a battery member such as a current collector mesh or net, a fastening component such as a screw, a bolt, or a rivet, a spring component such as a coil spring, an electric contact spring member such as a connector or a terminal, a structural component such as a shaft or a frame, a guide wire, a semiconductor bonding wire, and a winding wire used for a dynamo or a motor, or the like. Since the aluminum alloy material of the present disclosure has also excellent heat resistance, the aluminum alloy material is more suitable for the application particularly requiring heat resistance.

More specific application examples of the conductive member include a power electric wire such as an overhead power line, OPGW, a subterranean electric wire, or a submarine cable, a communication electric wire such as a telephone cable or a coaxial cable, an appliance electric wire such as a wired drone cable, a cab tire cable, an EV/HEV charge cable, a twisted cable for wind power on the ocean, an elevator cable, an umbilical cable, a robot cable, a train overhead wire, or a trolley wire, a transportation electric wire such as an automobile wire harness, a vessel electric wire, and an airplane electric wire, a bus bar, a lead frame, a flexible flat cable, a lightning rod, an antenna, a connector, a terminal, and a cable braid.

Examples of the battery member include a solar cell electrode.

More specific application examples of the structural component include a scaffold in a construction site, a conveyor mesh belt, a clothing metal fiber, a chain armor, a fence, an insect repellent net, a zipper, a fastener, a clip, aluminum wool, a bicycle component such as a brake or a spoke, a reinforcement wire made of tempered glass, a pipe seal, a metal packing, a protection reinforcing material for a cable, a fan belt cored bar, a wire for driving an actuator, a chain, a hanger, a sound isolation mesh, and a shelf board.

More specific application examples of the fastening component include a set screw, a staple, and a drawing pin.

More specific application examples of the spring component include a spring electrode, a terminal, a connector, a semiconductor probe spring, a blade spring, and a flat spiral spring.

The aluminum alloy material is suitable also as a metal fiber to be added in order to apply conductivity to a resin-based material, a plastic material, and a cloth or the like, and to control the strength and elastic modulus thereof.

The aluminum alloy material is suitable also as a consumer member and a medical member such as an eyeglass frame, a clock belt, a nib of a fountain pen, a fork, a helmet, or an injection needle.

In addition, the aluminum alloy having a high strength of the present disclosure is particularly suitably used as a metal conductor constituting a health care wearable device requiring high elasticity. A high material strength not easily causing plastic deformation, and good fatigue characteristics causing no fracture even under repeated deformation are required for the metal conductor. In particular, in a case in which the conductor unites the function of an electrode directly stuck on a human body, an aluminum alloy is preferably used as compared with a metal which is apt to cause allergy such as copper. Copper reacts with sweat or the like emitted from the human body, which disadvantageously causes occurrence of discoloration or rust. However, the aluminum alloy is advantageously less likely to cause such a problem.

Hereinbefore, embodiments of the present disclosure have been described. However, the present disclosure is not limited to the above embodiments, and includes all aspects included in the concept of the present disclosure and appended claims, and various modifications can be made within the scope of the present disclosure.

EXAMPLES

Next, Examples and Comparative Examples are described to further clarify the effects of the present disclosure. However, the present disclosure is not limited to these Examples.

Examples 1 to 17

First, bars having alloy compositions shown in Table 1 and each having a diameter of 10 mm were prepared. Next, aluminum alloy wire rods (diameter: 0.07 to 2.0 mm) were produced under manufacturing conditions shown in Table 1 using the bars.

Comparative Example 1

In Comparative Example 1, an aluminum wire rod (diameter: 0.24 mm) was produced under a manufacturing condition shown in Table 1 using a bar made of 99.99% by mass of Al and having a diameter of 10 mm.

Comparative Examples 2 to 9

In Comparative Examples 2 to 9, aluminum alloy wire rods (diameter: 0.07 to 2.0 mm) were produced under manufacturing conditions shown in Table 1 using bars having alloy compositions shown in Table 1 and each having a diameter of 10 mm.

Manufacturing conditions A to K shown in Table 1 are specifically as follows.

<Manufacturing Condition A>

The prepared bar was subjected to cold working [1] at a degree of working of 5.5. The bar was not subjected to refine annealing [2].

<Manufacturing Condition B>

The bar was subjected to cold working [1] under the same condition as the manufacturing condition A except that the degree of working of the cold working [1] was set to 6.5.

<Manufacturing Condition C>

The bar was subjected to cold working [1] under the same condition as the manufacturing condition A except that the degree of working of the cold working [1] was set to 7.5.

<Manufacturing Condition D>

The bar was subjected to cold working [1] under the same condition as the manufacturing condition A except that the degree of working of the cold working [1] was set to 10.0.

<Manufacturing Condition E>

The prepared bar was subjected to cold working [1] at a degree of working of 4.5, and then subjected to refine annealing [2] at a treatment temperature of 60° C. for a retention time of 1 hour.

<Manufacturing Condition F>

The bar was subjected to cold working [1] and refine annealing [2] under the same condition as the manufacturing condition E except that the degree of working of the cold working [1] was set to 5.5.

<Manufacturing Condition G>

The bar was subjected to cold working [1] and refine annealing [2] under the same condition as the manufacturing condition E except that the degree of working of the cold working [1] was set to 6.5.

<Manufacturing Condition H>

The bar was subjected to cold working [1] and refine annealing [2] under the same condition as the manufacturing condition E except that the degree of working of the cold working [1] was set to 10.0.

<Manufacturing Condition I>

The bar was subjected to cold working [1] under the same condition as the manufacturing condition A except that the degree of working of the cold working [1] was set to 3.5.

<Manufacturing Condition J>

The prepared bar was subjected to an aging precipitation heat treatment [0] at a treatment temperature of 180° C. for a retention time of 10 hours, and then subjected to cold working [1]. However, since breaking of wire occurred frequently, the work was stopped.

<Manufacturing Condition K>

The prepared bar was subjected to cold working [1]. However, since breaking of wire occurred frequently, the work was stopped.

Comparative Example 10 Manufacturing Condition P of Table 1

An Al bare metal for electricity was dissolved. Mg simple substance, an Al-25% by mass Si master alloy, an Al-6% by mass Fe alloy, an Al-50% by mass Cu master alloy, and an Al-10% by mass Cr master alloy were added thereto, and dissolved, to manufacture a molten metal having an alloy composition of Al-1.03Mg-0.90Si-0.20Fe-0.16Cu-0.15Cr. The molten metal was continuously cast and rolled by a belt-and-wheel type continuous casting rolling machine, to obtain a drawing stock having a diameter of 9.5 mm. The obtained drawing stock was subjected to solution water hardening at 520° C., an artificial aging treatment in which it was retained at 200° C. for 4 hours, wire drawing working at a working rate of 86.4% (degree of working: 2.0), and tempering at 140° C. for 4 hours, to obtain an aluminum alloy wire rod (diameter: 3.5 mm).

Comparative Example 11 Manufacturing Condition Q of Table 1

Aluminum for electricity having a purity of 99.8% was used, and an Al-6% by mass Fe master alloy, an Al-50% by mass Cu master alloy, an Al-20% by mass Si master alloy, and Mg simple substance were added thereto, to manufacture a molten metal having an alloy composition of Al-0.90% by mass Mg-0.80% by mass Si-0.20% by mass Fe-1.30% by mass Cu. A drawing stock (diameter: 18 mm) was obtained by belt-and-wheel type continuous casting rolling. The obtained drawing stock was subjected to first wire drawing working at a working rate of 47% (degree of working: 0.63), to set the diameter thereof to 9.5 mm, a solution treatment at 520° C. for 2 hours, and thereafter water hardening. The drawing stock was subjected to an aging treatment at 200° C. for 4 hours, second wire drawing working at a working rate of 86% (degree of working: 2.0), and a heat treatment at 140° C. for 4 hours, to obtain an aluminum alloy wire rod (diameter: 3.5 mm).

Comparative Example 12 Manufacturing Condition R of Table 1

From a molten metal having an alloy composition of Al-0.70% by mass Mg-0.69% by mass Si-1.01% by mass Fe-0.35% by mass Cu, a bar having a diameter of 10 mm was obtained by a Properzi type continuous casting rolling machine. The obtain bar was peeled so as to have a diameter of 9.5 mm. The bar was subjected to first wire drawing working at a degree of working of 2.6, a primary heat treatment at 300 to 450° C. for 0.5 to 4 hours, second wire drawing working at a degree of working of 3.6, a secondary heat treatment at 555° C. for 0.15 seconds in a continuous current heat treatment, and thereafter an aging heat treatment at 175° C. for 15 hours, to obtain an aluminum alloy wire rod (diameter: 0.43 mm).

Comparative Example 13 Manufacturing Condition S of Table 1

Into a graphite crucible, aluminum having a purity of 99.95% by mass, magnesium having a purity of 99.95% by mass, silicon having a purity of 99.99% by mass, and iron having a purity of 99.95% by mass were charged in predetermined amounts, and stirred and melted at 720° C. by high-frequency induction heating, to manufacture a molten metal having an alloy composition of Al-0.6% by mass Mg-0.3% by mass Si-0.05% by mass Fe. This was moved to a container provided with a graphite die, and subjected to continuous casting at a casting speed of about 300 mm/min via the water-cooled graphite die, to obtain a wire having a diameter of 10 mm and a length of 100 mm. A cumulative equivalent strain of 4.0 was introduced by the ECAP method. A recrystallization temperature obtained at this stage was 300° C. The wire was subjected to prior heating in an inactive gas atmosphere at 250° C. for 2 hours. Next, the wire was subjected to a first wire drawing treatment at a working rate of 29% (degree of working: 0.34). A recrystallization temperature obtained at this stage was 300° C. The wire was subjected to a primary heat treatment in an inactive gas atmosphere at 260° C. for 2 hours. Then, the wire was passed at a drawing speed of 500 mm/min in a water-cooled wire drawing die, to be subjected to a second wire drawing treatment at a degree of working of 9.3. A recrystallization temperature obtained at this stage was 280° C. The wire was subjected to a secondary heat treatment in an inactive gas atmosphere at 220° C. for 1 hour, to obtain an aluminum alloy wire rod (diameter: 0.08 mm).

[Evaluation]

The aluminum alloy wire rods according to the Examples and the Comparative Examples were subjected to evaluation of characteristics to be shown below. The evaluation conditions of the characteristics are as follows. The results are shown in Table 1.

[1] Alloy Composition

Measurement was performed by the emission spectrochemical analysis method according to JIS H1305: 2005. The measurement was performed using an emission spectrophotometer (manufactured by Hitachi High-Tech Science Corporation).

[2] Structure Observation

A metallographic structure was observed by scanning transmission electron microscopy (STEM) using a transmission electron microscope JEM-3100FEF (manufactured by JEOL Co., Ltd.). An observation sample to be used was cut at a cross section parallel to the longitudinal direction (wire drawing direction X) of the wire rod by focused ion beam (FIB) so as to have a thickness of 100 nm±20 nm, and finished by ion milling. In the STEM observation, a boundary in which contrasts were discontinuously different was recognized as a crystal grain boundary with the difference between contrasts as the orientation of a crystal using gray contrast. There may be no difference between gray contrasts even if crystal orientations are different depending on the diffraction condition of an electron beam. In that case, while an angle between the electron beam and the sample was changed by inclining by ±3 degrees by two sample rotational axes orthogonal to each other in a sample stage of an electron microscope, the observed surface was photographed under a plurality of diffraction conditions, to recognize the grain boundary. The observed field of view was set to (15 to 40) μm×(15 to 40) μm, and a center and a position near the middle of a surface layer (center side position separated by about ¼ of a wire diameter from the surface layer side) on a line corresponding to a wire diameter direction (direction perpendicular to a longitudinal direction) in the cross section were observed. The observed field of view was appropriately adjusted according to the size of a crystal grain. In the cross section parallel to the longitudinal direction (wire drawing direction X) of the wire rod, the presence or absence of the fibriform metallographic structure was determined from an image photographed during the STEM observation. FIG. 3 shows a part of the STEM image of the cross section parallel to the longitudinal direction (wire drawing direction X) of the wire rod of Example 14 photographed during the STEM observation. In the present Examples, the fibriform metallographic structure was estimated as “presence” in a case in which the metallographic structure as shown in FIG. 3 was observed. Furthermore, in each observed field of view, optional 100 crystal grains were selected. The size perpendicular to the longitudinal direction of each crystal grain and the size parallel to the longitudinal direction of the crystal grain were measured, to calculate the aspect ratio of the crystal grain. Furthermore, the average values of the size perpendicular to the longitudinal direction of the crystal grains and the aspect ratios were calculated from the total of the observed crystal grains. In a case in which the observed crystal grains were clearly larger than 400 nm, the number of selection of the crystal grains whose size was measured was reduced, and the average value thereof was calculated. In a case in which the size parallel to the longitudinal direction of the crystal grains was clearly 10 or more times the size perpendicular to the longitudinal direction of the crystal grains, the crystal grains were determined to uniformly have an aspect ratio of 10 or more.

[3] Tensile Strength

According to JIS Z2241: 2001, a tensile test was performed using a precision universal tester (manufactured by Shimadzu Corporation), to measure a tensile strength (MPa). The test was carried out under conditions of a distance between marks of 10 cm and a deformation speed of 10 mm/min. Three of the wire rods directly manufactured under the manufacturing conditions A to S and three of the wire rods further heated at 110° C. for 24 hours after manufacturing were subjected to the tensile test, and the average values (N=3) thereof were defined as a tensile strength before heating, and a tensile strength after heating. In the present examples, the wire rods before heating, having a tensile strength of 480 MPa or more were considered to be at a pass level. The wire rods after heating, having a tensile strength of 480 MPa or more were defined as “very good”. The wire rods after heating, having a tensile strength of less than 480 MPa and 420 MPa or more were defined as “good”. The wire rods after heating, having a tensile strength of less than 420 MPa were defined as “poor”.

[4] Vickers Hardness (HV)

According to JIS Z 2244: 2009, a Vickers hardness (HV) was measured using a microhardness tester HM-125 (manufactured by Akashi Corporation (current Mitutoyo Corporation)). At this time, a test force was set to 0.1 kgf, and a retention time was set to 15 seconds. Measurement positions were a center and a position near the middle of a surface layer (center side position separated by about ¼ of a wire diameter from the surface layer side) on a line corresponding to a wire diameter direction (direction perpendicular to a longitudinal direction) in the cross section parallel to the longitudinal direction of the wire rod. The average value (N=5) of the measured values was defined as the Vickers hardness (HV) of the wire rod. In a case in which the difference between the maximum value and the minimum value of the measured values was 10 or more, the number of measurements was further increased, and the average value (N=10) was defined as the Vickers hardness (HV) of the wire rod. The Vickers hardness (HV) was preferably greater, and the Vickers hardness of 125 or more was considered to be at a pass level in the present Examples.

TABLE 1 Evaluation of structure Evaluation of characteristics Alloy composition [% by mass] Size Tensile One or more selected perpendicular strength (TS) from Cu, Ag, Zn, Ni, Co, Au, Al and Fibriform to longitudinal Before After Vickers Mn, Cr, V, Zr, and Sn inevitable Manufacturing metallographic direction of Aspect heating heating hardness Mg Si Fe 1 2 3 total Sc impurities condition structure crystal grains ratio [MPa] [MPa] (HV) Examples 1 0.63 0.61 0.21 Cu 0.07 — — 0.07 — Balance B Presence 170 nm >10 540 Very good 148 2 0.63 0.61 0.21 Cu 0.11 Au 0.11 — 0.22 — Balance B Presence 150 nm >10 560 Very good 150 3 0.63 0.61 0.21 Cu 1.21 Ag 0.71 — 1.92 — Balance F Presence 150 nm >10 560 Very good 151 4 0.63 0.61 0.21 Cu 0.71 Ni 0.32 — 1.03 — Balance H Presence  90 nm >10 650 Very good 170 5 0.63 0.61 0.21 Ag 0.12 — — 0.12 — Balance B Presence 180 nm >10 530 Very good 142 6 0.63 0.61 0.21 Ag 0.55 Sn 0.05 — 0.60 — Balance D Presence  70 nm >10 640 Very good 170 7 0.63 0.61 0.21 Ag 0.35 V 0.08 — 0.43 — Balance G Presence 130 nm >10 580 Very good 155 8 0.63 0.61 0.21 Zn 0.11 Zr 0.06 — 0.17 — Balance A Presence 220 nm >10 510 Good 137 9 0.63 0.61 0.21 Co 0.11 Mn 0.11 — 0.22 — Balance E Presence 250 nm >10 490 Good 128 10 0.18 1.95 0.11 Zn 0.13 — — 0.13 — Balance G Presence 120 nm >10 640 Very good 168 11 0.22 0.22 0.15 Cu 0.07 Cr 0.07 — 0.14 — Balance C Presence 160 nm >10 560 Good 149 12 0.63 0.61 1.42 Cu 0.07 Sn 0.04 — 0.11 — Balance C Presence 100 nm >10 610 Very good 160 13 0.91 0.88 0.15 Cu 0.07 — — 0.07 — Balance D Presence  90 nm >10 690 Very good 180 14 0.98 0.60 0.07 Cu 0.28 Cr 0.14 — 0.42 — Balance C Presence  80 nm >10 575 Very good 150 15 1.76 0.31 0.11 Ag 0.12 — — 0.12 — Balance H Presence  80 nm >10 650 Very good 170 16 0.98 0.58 0.02 Cu 0.28 Cr 0.14 — 0.42 — Balance B Presence 150 nm >10 550 Very good 152 17 0.95 1.12 0.31 Cu 0.91 Mn 0.65 Zn 0.38 1.94 — Balance B Presence 160 nm >10 560 Very good 160 Comparative Examples 1 — — — — — Balance C Absence   0.8 μm 5 150 Poor   43 2 0.17 0.17 0.21 Cu 0.07 — 0.07 — Balance A Absence 340 nm >10 380 Poor 103 3 — 0.02 0.03 — 0.31 Balance C Absence   0.4 μm >10   58 Poor 210 4 0.63 0.61 0.21 — — Balance B Presence 190 nm >10 530 Poor 143 5 1.82 2.11 0.21 Cu 0.07 — 0.07 — Balance K — — — — — — 6 0.91 0.88 1.62 Cu 0.07 — 0.07 — Balance K — — — — — — 7 0.63 0.61 0.21 Cu 1.81 Zr 0.28 2.09 — Balance K — — — — — — 8 0.63 0.61 0.21 Cu 0.07 — 0.07 — Balance J — — — — — — 9 0.63 0.61 0.21 Cu 0.07 — 0.07 — Balance I Absence   0.5 μm >10 420 Poor 117 10 1.03 0.90 0.20 Cu 0.16 Cr 0.15 0.31 — Balance P Absence   0.5 μm >10 440 Poor 122 11 0.90 0.80 0.20 Cu 1.30 — 1.30 — Balance Q Absence   0.5 μm >10 470 Poor 130 12 0.70 0.69 1.01 Cu 0.35 — 0.35 — Balance R Absence   4 μm 2 320 Poor   91 13 0.60 0.30 0.05 — — Balance S Absence   0.5 μm >10 260 Poor   75 (Note) Underlined bold characters in Table show wire rods outside the appropriate range of the present invention and wire rods of which evaluation results do not reach the pass level in the present Examples.

From the results of Table 1, it was confirmed that the aluminum alloy wire rod according to each of Examples 1 to 17 of the present disclosure has a specific alloy composition, and the aluminum alloy wire rod has a fibriform metallographic structure where crystal grains extend so as to be aligned in one direction; and in a cross section parallel to the one direction, a size perpendicular to a longitudinal direction of the crystal grains is 270 nm or less. FIG. 3 shows the STEM image of the cross section parallel to the wire drawing direction of the aluminum alloy wire rod according to Example 14. The same metallographic structure as that of FIG. 3 was confirmed also in the cross section parallel to the longitudinal direction of the aluminum alloy wire rod according to each of Examples 1 to 13 and 15 to 17. It was confirmed that the aluminum metal wire rod according to each of Examples 1 to 17 of the present disclosure having such a specific metallographic structure exhibits a high strength comparable to that of an iron-based or copper-based metal material (for example, tensile strength: 480 MPa or more, Vickers hardness (HV): 125 or more). Since the aluminum metal wire rod according to each of Examples 1 to 15 of the present disclosure contains at least one or more selected from Cu, Ag, Zn, Ni, Co, Au, Mn, Cr, V, Zr, and Sn in predetermined amounts, the aluminum metal wire rod was confirmed to have a high tensile strength maintained even after heating and excellent heat resistance.

On the other hand, particularly, the aluminum metal wire rod of Comparative Example 4 not containing Cu, Ag, Zn, Ni, Co, Au, Mn, Cr, V, Zr, and Sn was confirmed to have a tensile strength largely decreased after heating, and poorer heat resistance than that of the aluminum alloy wire rod of each of Examples 1 to 17 according to the present disclosure.

It was confirmed that the alloy composition of the aluminum alloy wire rod of each of Comparative Examples 1 to 3 and 9 to 13 does not satisfy the appropriate range of the present disclosure, or does not have a fibriform metallographic structure where crystal grains extend so as to be aligned in one direction; and a size perpendicular to a longitudinal direction of the crystal grains is also 500 nm or more. It was confirmed that the aluminum alloy wire rod of each of Comparative Examples 1 to 3 and 9 to 13 has a remarkably poorer tensile strength and Vickers hardness (HV) than those of the aluminum alloy wire rod of each of Examples 1 to 15 according to the present disclosure.

Since the alloy composition of the wire rod in each of Comparative Examples 5 to 7 did not satisfy the appropriate range of the present disclosure, working cracks were confirmed to occur in wire drawing working [1]. Since an aging precipitation heat treatment [0] was performed before the wire drawing working [1] in Comparative Example 8, working cracks were confirmed to occur during the wire drawing working [1] performed at a high degree of working in order to increase the crystal grain boundary. 

What is claimed is:
 1. An aluminum alloy material comprising an alloy composition consisting of 0.2 to 1.8% by mass of Mg, 0.2 to 2.0% by mass of Si, 0.01 to 1.50% by mass of Fe, 0.06 to 2% by mass in total of at least one selected from Cu, Ag, Zn, Ni, Co, Au, Mn, Cr, V, Zr, and Sn, with the balance containing Al and inevitable impurities, wherein the aluminum alloy material has a fibriform metallographic structure where crystal grains extend so as to be aligned in one direction; and in a cross section parallel to the one direction, an average value of a size perpendicular to a longitudinal direction of the crystal grains is 270 nm or less.
 2. The aluminum alloy material according to claim 1, wherein an aspect ratio of the crystal grains is in excess of
 10. 3. The aluminum alloy material according to claim 1, wherein the aluminum alloy material has a Vickers hardness (HV) of 125 to
 250. 4. A conductive member comprising the aluminum alloy material according to claim
 1. 5. A battery member comprising the aluminum alloy material according to claim
 1. 6. A fastening component comprising the aluminum alloy material according to claim
 1. 7. A spring component comprising the aluminum alloy material according to claim
 1. 8. A structural component comprising the aluminum alloy material according to claim
 1. 